某型飞机发动机喷口电磁阀测试系统的设计  

Test-system Design of Nozzle Solenoid Valve for the Certain Aero-engine

作　　者：张伟[1] 任再青[1] 

机构地区：[1]空军第一航空学院航空机械工程系,河南信阳464000

出　　处：《液压气动与密封》2015年第10期34-36,共3页Hydraulics Pneumatics & Seals

摘　　要：根据飞机发动机喷口电磁阀的测试需求,设计了电磁阀的测试系统。该系统由液压测控单元,电子测量单元,软件控制单元组成。可以对喷口电磁阀密封性能、溢流性能、工作性能参数测量。试验结果表明:测试系统满足航修厂对喷口电磁阀的测试需求,在应用中取得良好效果。Based on the test requirement of hydraulic solenoid valve of exhaust nozzle exit of a certain aero-engine, the test-system of the hy- draulic solenoid valve is designed. The test-system consists of hydraulic measurement and control unit, a electronic measurement unit and a software control unit. It can be used to perform the performance parameter test of the hydraulic solenoid valve.The test-system is fulfilled the needs of fighter repair factories and worked in good condition.

关 键 词：发动机 电磁阀 测试系统 设计 

分 类 号：TH137[机械工程—机械制造及自动化]